Gas Turbine Laboratory: Recent submissions

Now showing items 10-12 of 123

    • Blade passage flow structure effects on axial compressor rotating stall inception 

      Hoying, Donald Andrew (Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1996], 1996)
      A new computational approach has been developed to study the inception of rotating stall in axial compressors. Using this approach the flow structures within the compressor blade passages have been examined in order to ...

    • A numerical investigation of a flutter in a transonic fan 

      Isomura, Kousuke (Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1996], 1996)
      The mechanism of the bending mode flutter of a modern transonic fan has been studied using a quasi-3D viscous unsteady code. The type of flutter in the scope of this research is that for a highly loaded blade with a tip ...

    • Rotor wake behavior in a transonic compressor stage and its effect on the loading and performance of the stator 

      Durali, Mohammad (Cambridge, Mass. : Gas Turbine & Plasma Dynamics Laboratory, Massachusetts Institute of Technology, [1980], 1980)
      The structure and behavior of wakes from a transonic compressor rotor and their effects on the loading and performance of the downstream stator have been studied experimentally. The rotor is 2 feet in diameter with a tip ...